NII Mash N2O4/UDMH rocket engine. In Production. Experimental low-thrust thruster. Chamber from niobium alloy. Chamber pressure 41 / 17 bar. Specific impulse 313 / 302,3 sec.
Status: In Production. Thrust: 0.40 N (0.08 lbf). Unfuelled mass: 0.10 kg (0.22 lb). Specific impulse: 290 s.
Engine: 0.10 kg (0.22 lb). Chamber Pressure: 41.00 bar. Thrust to Weight Ratio: .4.